Transcription
Pilot's Operating HandbookAnd FAA ApprovedAirplane Flight ManualSKYLANEf)Member of GAMA----:M o-:d-e':""l 1 82 T ----'NAV III Avionics - GFC 700 AFCSSERIAL NUMBER/52 B 2.085'"REGISTRATION NUMBERNb2'13i VU - ROeSerials 18281869 and18281876 and OnThis publication includes the material required to be furnished to the pilot by 14 CFR 23.eo.APPROVED BYDATE OF APPROVALCOPYRIGHT 2006CESSNA A IRCRAFT COMPANYW ICHITA, KANSAS, USA182TPHBUS-03 A-I:DiII.(: '21 Ocfoller 2()CJ&ORIGINAL ISSUE - 27 OCTOBER 2006REVIS ION 3 - 22 NOVEMBER 2010U.S.
THIS MANUAL WAS PROVIDED FOR THEAIRPLANE IDENTIFIED ON THE TITLEPAGEONSUBSEQUENT REVISIONS SUPPLIED BYCESSNA AIRCRAFT COMPANY MUST BEPROPERLY INSERTED.Cessna Aircraft Company
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSPILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALCESSNA MODEL 182TNAV III AVIONICS OPTION - GFC 700 AFCSSERIALS18281869 AND 18281876 AND ONORIGINAL ISSUE - 27 OCTOBER 2006REVISION 3 - 22 NOVEMBER 2010PART NUMBER: 182TPHBUS-03182TPHBUS-03U.S.ilii
CESSNAMODEL 182T NAV IIIGFC 700 AFCSINTRODUCTIONCONGRATULATIONSCongratulations on your purchase and welcome to Cessna ownership!Your Cessna has been designed and constructed to give you the mostin performance, value and comfort.This Pilot's Operating Handbook has been prepared as a guide to helpyou get the most utility from your airplane. It contains information aboutyour airplane's equipment, operating procedures, performance andsuggested service and care. Please study it carefully and use it as areference.The worldwide Cessna Organization and Cessna Customer Serviceare prepared to serve you. The following services are offered by eachCessna Service Station: THE CESSNA AIRPLANE WARRANTIES, which provide coveragefor parts and labor, are upheld through Cessna Service Stationsworldwide. Warranty provisions and other important information arecontained in the Customer Care Program Handbook supplied withyour airplane. The Customer Care Card assigned to you at deliverywill establish your eligibility under warranty and should bepresented to your local Cessna Service Station at the time ofwarranty service . FACTORY TRAINED PERSONNEL to provide you with courteous,expert service. FACTORY APPROVED SERVICE EQUIPMENT to provide youefficient and accurate workmanship. A STOCK OF GENUINE CESSNA SERVICE PARTS are availablewhen you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICINGCESSNA AIRPLANES. Cessna Service Stations have all of thecurrent Maintenance Manuals, Illustrated Parts Catalogs andvarious other support publications produced by Cessna AircraftCompany.A current Cessna Service Station Directory accompanies your newairplane. The Directory is revised annually, and a current copy can beobtained from your nearest Cessna Service Station.We urge all Cessna owners/operators to utilize the benefits availablewith in the Cessna Organization.182TPHBUS-00U.S.iii
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700AFCSPERFORMANCE - SPECIFICATIONS*SPEEDMaximum at Sea Level . . . . . . . . 150 KNOTSCruise, 80% Power at 7000 Feet. . . . . . 145 KNOTSCRUISE - Recommended lean mixture with fuel allowance for enginestart, taxi, takeoff, climb and 45 minutes reserve.80% Power at 7000 Feet . . . . . . . . . . Range - 773 NM87 Gallons Usable Fuel. . . . . . . . . . Time - 5.4 HOURS75% Power at 8000 Feet . . . . . . . . Range - 813 NM87 Gallons Usable Fuel. . . . . . . Time - 5.8 HOURSMax Range at 10,000 Feet, 55% Power . . . Range - 930 NM87 Gallons Usable Fuel. . . . . . . Time - 7.6 HOURSRATE OF CLIMB AT SEA LEVEL: . . . . . . . . 924 FPMSERVICE CEILING: . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18,100 FEETTAKEOFF PERFORMANCE:Ground Roll . . . . . . . . 795 FEETTotal Distance Over 50 Foot Obstacle . 1514 FEETLANDING PERFORMANCE:Ground Roll . . . . . . . . . . . . . . 590 FEETTotal Distance Over 50 Foot Obstacle . . . . . 1350 FEETSTALL SPEED (KCAS):Flaps UP, Power Idle . . . . . 54 KCASFlaps FULL, Power Idle . .49 KCAS(Continued Next Page)ivU.S.182TPHBUS-00
CESSNAMODEL 182T NAV IIIGFC 700 AFCSINTRODUCTIONPERFORMANCE - SPECIFICATIONS(Continued)MAXIMUM WEIGHT:Ramp . . . 3110 POUNDSTakeoff . . . . . . . . . . . . . . 3100 POUNDSLanding . . . . . . . . . . . . 2950 POUNDSSTANDARD EMPTY WEIGHT: . . . . . . . . 1924 POUNDSMAXIMUM USEFUL LOAD: . . . . . . . . . . . . . . . 1186 POUNDSBAGGAGE ALLOWANCE: . . . . . . . 200 POUNDSWING LOADING : . . . . . . . 17.8 Ibs/sq. ft.POWER LOADING : . . . . . . . . . . . . 13.5 Ibs/HPFUEL CAPACITY: . . . . . . . . . . . 92 GALLONSOIL CAPACITY: . . . . . . . . . . . . . 9 QUARTSENGINE: Textron Lycoming . . . . . . . . . . . IO-540-AB1A5230 BHP at 2400 RPMPROPELLER: 3-Bladed, Constant Speed, Diameter . . . 79 INCHESNOTE*Speed performance and range are shown for an airplaneequipped with the standard wheel and brake fairings.These fairings increase the speeds approximately 3 knotsover an airplane without the fairings .The above performance figures are based on the indicated weights,standard atmospheric conditions, level, hard-surfaced dry runways andno wind. They are calculated values derived from flight tests conductedby Cessna Aircraft Company under carefully documented conditionsand will vary with individual airplanes and numerous factors affectingflight performance.182TPHBUS-00U.S.v
CESSNAMODEL 182T NAV IIIGFC 700AFCSINTRODUCTIONCOVERAGEIThe Pilot's Operating Handbook (POH) in the airplane at the time ofdelivery from Cessna Aircraft Company contains information applicableto the Model 182T Nav III airplanes by serial number and registrationInumber shown on the Title Page. This POH is applicable to 182Tairplanes , Serials 18281869 and 18281876 and On, equipped with theNAV III Avionics Option and Garmin GFC 700 Automatic Flight ControlSystem (AFCS). All information is based on data available at the time ofpublication.This POH consists of nine sections that cover all operational aspects ofa standard equipped airplane. Section 9 contains the supplementswhich provide amended operating limitations, operating procedures,performance data and other necessary information for airplanesconducting special operations for both standard and optionalequipment installed in the airplane.Supplements are individual documents, and may be issued or revisedwithout regard to revision dates which apply to the POH itself. Thesesupplements contain a Log of Effective Pages, which should be used todetermine the status of each supplement.viU.S.182TPHBUS-01
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSORIGINAL ISSUE AND REVISIONSThis Pilot's Operating Handbook and FM Approved Airplane Flight- Manual is comprised of the original issue and any subsequentrevisions . To make sure that information in this manual is current, therevisions must be incorporated as they are issued . As revisions areissued , they will be noted in the Log of Effective Pages .The part number of this manual has also been designed to further aidthe owner/operator in determining the revision level of any POH . Referto the example below for a breakdown:182TPHBUS-00-.:::. Revision Level (Original Issue)Manual (Pilot's Operating HandbookNav III GFC 700 AFCS, U.S.)(Serials 18281869 and 18281876 andOn)L.--------Airplane Model- (182T)1.-lit is the responsibility of the owner to maintain this POH in a currentstatus when it is being used for operational purposes . Owners shouldcontact a Cessna Service Station whenever the revision status of theirPOH is in question.Revisions are distributed to owners of U.S. Registered aircraftaccording to FM records at the time of revision issuance, and toInternationally Registered aircraft according to Cessna Owner Advisoryrecords at the time of issuance. Revisions should be read carefullyupon receipt and incorporated in this POH.182TPHBUS-01U.S.vii
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700AFCSREVISION FILING INSTRUCTIONSREGULAR REVISIONSPages to be removed or inserted in the Pilots' Operating Handbook andFAA Approved Airplane Flight Manual are determined by the Log ofEffective Pages located in this section. This log contains the pagenumber and revision level for each page within the POH. As revisionsto the POH occur, the revision level on effected pages is updated.When two pages display the same page number, the page with thelatest revision level shall be inserted into the POH. The revision levelon the Log Of Effective Pages shall also agree with the revision level ofthe page in question.TEMPORARY REVISIONSUnder limited circumstances, temporary revisions to the POH may beissued. These temporary revisions are to be filed in the applicablesection in accordance with filing instructions appearing on the first pageof the temporary revision.Temporary Revisions will remain current until they have either beenincorporated into the next POH revision or another temporary revisionhas been issued that supersedes that temporary revision. Eachtemporary revision is issued with a current List of Temporary Revisionsthat is to be inserted opposite the first page of the Log of EffectivePages in the front of the POH and will supersede any previously issuedList of Temporary Revisions. This list is used to track the status oftemporary revisions issued against this POH and is to be removed anddiscarded at the next revision to the POH. Removal of temporaryrevisions from the POH is accomplished per the removal instructionson each temporary revision.viiiU.S.182TPHBUS-01
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSIDENTIFYING REVISED MATERIALA bar will extend the full length of deleted, new, or revised text addedon new or previously existing pages. This bar will be located adjacent tothe applicable text in the margin on the left side of the page.A bar in the footer will indicate a revision to the header/footer, a newpage, format or spelling/grammar changes and/or that information hasslipped to or from that page .A bar located adjacent to the figure number in the margin on the leftside of the page will be used to indicate that the figure number only haschanged.An asterisk located at the end of a figure number will be used toindicate that an illustration has been revised or is all new material (Ex:Figure 3-4*).All revised pages will carry the revision number opposite the pagenumber on the applicable page. A list of revisions is located at thebeginning of the Log Of Effective Pages .I 182TPHBUS-03U.S.ix
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700AFCSWARNINGS, CAUTIONS AND NOTESThroughout the text, warnings, cautions and notes pertaining toairplane handling and operations are utilized. These adjuncts to the textare used to highlight or emphasize important points.WARNINGOPERATING PROCEDURES, TECHNIQUES, ETC.,WHICH CAN RESULT IN PERSONAL INJURY OR LOSSOF LIFE IF NOT CAREFULLY FOLLOWED.CAUTIONOPERATION PROCEDURES, TECHNIQUES , ETC.,WHICH CAN RESULT IN DAMAGE TO EQUIPMENT IFNOT CAREFULLY FOLLOWED .NOTEAn operating procedure, technique,considered essential to emphasize .U.S.etc.,whichis182TPHBUS-03
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSLOG OF EFFECTIVE PAGESUse this page to determine the currency and applicability of your POH.Pages affected by the current revision are indicated by an asterisk (*)preceding the pages listed under the Page Number column.Date of IssueRevision LevelDate of IssueRevision LevelOriginal Issue27 October 2006Revision 215 December 2008Revision 120 December 2007 Revision 322 November 2010PageNumberPageStatusRevisionNumber* TitleAssignment RecordRevisedOriginalo* i/iiiii thru vvi thru viii* ix th ru xv/xvi* xvii/xviii thru xix/xxRevisedOriginalRevisedRevisedAdded1-1/1-2* ginalRevisedAdded1-41-51-6 thru 1-81-91-101-11 thru 1-281-29/1-302-1/2-22-3 thru 2-52-62-7* 2-8 thru do2o3(Continued Next Page)I 182TPHBUS-03U.S.xi
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700AFCSLOG OF EFFECTIVE PAGESPageNumber2-10 2-122-132-15 2-172-202-212-25PageStatusthru 2-11thru 2-24thru ginalRevised3-13-23-3/3-43-5 thru 3-63-73-8 thru 3-113-12 thru 3-213-223-233-24 thru 3-263-273-28 thru 3-313-323-33 3-343-35 th ru dOriginalRevisedOriginal 4-1 thru 4-24-3 4-44-5 thru 4-6 4-74-8 4-9 thru dRevisedRevisedthru 2-14thru 2-16thru 13o3132(Continued Next Page)I xiiu.S.182TPHBUS-03
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSLOG OF EFFECTIVE edOrig inal31010302323205-1 /5-2 thru 5-85-95-10 thru 5-13 5-145-15 thru 1 /6-26-3 thru 6-46-5 thru 6-106-116-12 thru 6-15 6-16 thru 6-17/6-186-19 6-206-216-22 ginalRevisedRevisedRevisedOrig inalRevisedRevisedRevisedRevised 4-13 thru4-174-184-19 thru4-21 4-224-23 thru4-27 4-28 thru4-30 4-314-32 thru4-41 thru4-43 (Continued Next Page)I 182TPHBUS-03U.S.xiii
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSLOG OF EFFECTIVE PAGESPageNumber 7-17-2 thru 7-3/7-47-57-6 thru 7-107-117-127-13 thru 7-217-227-23 thru 7-247-257-267-277-28 thru 7-297-30 thru 7-317-32 thru 7-367-377-38 thru 7-417-427-43 thru 7-467-477-48 thru 7-497-507-517-527-537-547-557-56 thru 7-587-597-607-617-62 thru 7-667-67 thru 1o31323o1o1o31oo3o3o3o3o3o3(Continued Next Page)U.S.182TPHBUS-03
CESSNAMODEL 182T NAV IIIGFC 700 AFCSINTRODUCTIONLOG OF EFFECTIVE 7-70 thru 7-717-727-73 thru 7-76* 7-777-78 thru 7-80* 7-81 thru 7-827-83 thru RevisedRevisedAddedo8-1 thru 8-28-3 thru 8-58-68-7 thru 8-88-9* 8-108-118-128-13 thru 8-198-208-218-228-23 thru PPROVEDBY For Carlos Ayala. Acting Lead ODA AdministratorCessna Aircraft CompanyOrganization Delegation Authorization ODA-l00129-CEFAA Approved Under 14 CFR Part 183 Subpart DDATE OF APPROVAL 7Z-Nc.ve. . be "I 182TPHBUS-03z.o 10U.S.xv/xvi
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSSERVICE BULLETIN CONFIGURATION LISTThe following is a list of Service Bulletins that are applicable to theoperation of the airplane, and have been incorporated into this manual.This list contains only those Service Bulletins that are currently active .INumberTitleAirglane SerialEffectivit B08-34-03 Forward LookingRevision IncorgoratedIncomorated in Aimlane18281869 and18281876 thru182821292SB09-34-05 Garmin G1000 System 18281869 andSoftware Upgrade to18281876 thru563.14182820453ITerrain Avoidance(FLTA) Alert Over TheOpen Ocean/SeaI 182TPHBUS-03U.S.xvii/xviii
INTRODUCTIONCESSNAMODEL 182T NAV IIIGFC 700 AFCSTABLE OF CONTENTSSECTIONGENERAL . 1LIMITATIONS .2EMERGENCY PROCEDURES . 3NORMAL PROCEDURES . .4PERFORMANCE . 5WEIGHT AND BALANCE/EQUIPMENT LIST . . 6AIRPLANE AND SYSTEM DESCRIPTION . 7HANDLING, SERVICE AND MAINTENANCE . 8SUPPLEMENTS . 9I 182TPHBUS-03U.S.xix/xx
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALGENERALTABLE OF CONTENTSPageThree View - Normal Ground Attitude . . . . . . . 1-3Introduction . . . . . . . . . . . . . . . . 1-5Descriptive Data . . . . . . . . . . . 1-5Engine . . . . . . . . . . . . . . . . 1-5Propeller . . . . . . . . . . . . . . . . . 1-5Fuel . . . . . . . . . . . . . . . . . . . . 1-6Fuel Capacity . . . . . . . . . . . . . . . . . 1-6Oil . . . . . . . . . . . . . . . . . 1-7Oil Specification . . . . . . . . . . . . . . 1-7Oil Capacity . . . . . . . . . . . . . . . . . . . . . . . 1-7Maximum Certificated Weights . . . . . . . . . . . . 1-8Weight In Baggage Compartment - Normal Category . . . 1-8Standard Airplane Weights . . . . . . . . . . . . . . . . . . . 1-8Cabin And Entry Dimensions . . . . . . . . . . . . 1-8Baggage Space And Entry Dimensions . . . . . . . 1-8Specific Loadings . . . . . . . . . . . . . . . 1-8Symbols, Abbreviations And Terminology . . . . . . . . 1-9General Airspeed Terminology And Symbols . . . . . . . 1-9Meteorological Terminology . . . . . . . . . . . 1-10Engine Power Terminology . . . . . . . . . . . . . 1-10Airplane Performance And Flight Planning Terminology . 1-12Weight And Balance Terminology . . . . . . . . . . . . 1-13Metric/lmperial/U .S. Conversion Charts . . . . . . . . . . 1-15Weight Conversions . . . . . . . . . . . . . . . 1-16Length Conversions . . . . . . . . . . . 1-18Distance Conversions . . . . . . . . . . . . 1-22Volume Conversions . . . . . . . . . . . . . . . 1-23Temperature Conversions . . . . . . . . . . . 1-26Pressure Conversion . . . . . . . . . . . . . . . 1-27Volume To Weight Conversion . . . . . . . . . . . . 1-28Quick Conversions . . . . . . . . . . . . . 1-29/1 -30182TPHBUS-01U.S.1-1/1-2
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALTHREE VIEW - NORMAL GROUND ATTITUDE63143i'*r--------36'-0"-------- ; Pt 070ST1032Figure 1-1 * (Sheet 1 of 2)182TPHBUS-03U.s.1-3
SECTION 1GENERALCESSNAMODEL 182T NAV IIIGFC 700AFCSTHREE VIEW - NORMAL GROUND ATTITUDEt-------29'-0" --- t r9'- 4"NOTE Wing span shown with standard strobe lights installed . Wheel base length is 66 .5 inches. Propeller ground clearance is 10.875 inches. Wing area is 174.0 square feet. Minimum turning radius (*pivot point to outboard wingtip) is 27.0 feet. Normal ground attitude is shown with nose strut showingapproximately 2 inches of strut, and wings level.Figure 1-1 (Sheet 2)1-4U.S.182TPHBUS-00
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALINTRODUCTIONThiS POH contains 9 sections, and includes the material required to befurnished to the pilot by 14 CFR 23. It also contains supplemental datasupplied by Cessna Aircraft Company.ISection 1 provides basic data and information of general interest. Italso contains definitions or explanations of symbols, abbreviations, andterminology commonly used.DESCRIPTIVE DATAENGINENumber of Engines : 1Engine Manufacturer: Textron LycomingEngine Model Number: IO-540-AB1A5Engine Type: Normally aspirated, direct drive, air-cooled, horizontallyopposed, fuel injected, six cylinder engine with 541 .5 cu.in . displacement.Horsepower Rating and Engine Speed: 230 rated BHP at 2400 RPMPROPELLERPropeller Manufacturer: McCauley Propeller SystemsPropeller Model Number: B3D36C431/80VSA-1Number of Blades: 3Propeller Diameter: 79 inchesPropeller Type: Constant speed and hydraulically actuated .(Continued Next Page)182TPHBUS-01U.S.1-5
CESSNAMODEL 182T NAV IIIGFC 700AFCSSECTION 1GENERALDESCRIPTIVE DATA(Continued)FUELWARNINGUSE OF UNAPPROVED FUELS MAY RESULT INDAMAGE TO THE ENGINE AND FUEL SYSTEMCOMPONENTS, RESULTING IN POSSIBLE ENGINEFAILURE.Approved Fuel Grades (and Colors):100LL Grade Aviation Fuel (Blue)100Grade Aviation Fuel (Green)NOTEIsopropyl alcohol or Diethylene Glycol Monomethyl Ether(DiEGME) may be added to the fuel supply. Additiveconcentrations shall not exceed 1% for isopropyl alcohol or0 .10% to 0.15% for DiEGME. Refer to Section 8 foradditional information .FUEL CAPACITYTotal Capacity . . . . . . . . . . . . . .92.0Total Usable . . . . . . . . . . . 87.0Total Capacity Each Tank . . . . . . .46.0Total Usable Each Tank . . . . OTETo ensure maximum fuel capacity and minimizecrossfeeding when refueling, always park the airplane in awings level, normal ground attitude and place the fuelselector in the LEFT or RIGHT position. Refer to Figure 1-1for normal ground attitude dimensions.(Continued Next Page)1-6U.S.182TPHBUS-00
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALDESCRIPTIVE DATA(Continued)OILOIL SPECIFICATIONMIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil: Usedwhen the airplane was delivered from the factory and should be used toreplenish the supply during the first 25 hours . This oil should be drainedand the filter changed after the first 25 hours of operation. Refill theengine with MIL-L-6082 or SAE J1966 Aviation Grade Straight MineralOil and continue to use until a total of 50 hours has accumulated or oilconsumption has stabilized .MIL-L-22851 or SAE J1899 Aviation Grade Ashless Dispersant Oil: Oilconforming to Textron Lycoming Service Instruction No 1014, and allrevisions and supplements thereto, must be used after first 50 hoursor oil consumption has stabilized.Recommended viscosity for temperature range:TemperatureMIL-L-6082MIL-L-22851or SAE J1966or SAE J1899Straight Mineral Oil Ashless Dispersant OilSAE GradeSAE GradeAbove 2rC (80 F)6060Above 16 C (60 F)SO40 or SO1 C (30 F) to 32 C (90 F)4040-18 C (O F) to 21 C (70 F)3030, 40 or 20W-40Below -12 C (10 F)-18 C (O F) to 32 C (90 F)All Temperatures2030 or 20W-3020W-SO20W-SO or 1SW-SO--1SW-SO or 20W-SONOTEWhen operating temperatures overlap, use the lightergrade of oil.OIL CAPACITYSump . . . . . . 8 U.S. QUARTSTotal. . . . . . . . . . . . . . . . 9 U.S. QUARTS(Continued Next Page)182TPHBUS-00U.S.1-7
SECTION 1GENERALCESSNAMODEL 182T NAV II IGFC 700AFCSDESCRIPTIVE DATA(Continued)MAXIMUM CERTIFICATED WEIGHTSRamp Weight . . . . . . . . . . . . . . . 31 10 POUNDSTakeoff Weight . . . . . . . . . . . . . . . . 3100 POUNDSLanding Weight . . . . . . . . . . 2950 POUNDSWEIGHT IN BAGGAGE COMPARTMENT, NORMAL CATEGORYBaggage Area A (Station 82 to 109) . . . . . . . 120 POUNDS· . . . . . . . . . . . . . . . . . . . . . . Refer to note below.Baggage Area B (Station 109 to 124) . . . . . . . . . . 80 POUNDS· . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to note belowBaggage Area C (Station 124 to 134) . . . . 80 POUNDS· . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to note belowNOTEThe maximum allowable comb ined we ight capacity forbaggage in areas A, Band C is 200 pounds. The maximumallowable weight capacity for baggage in areas Band C is80 pounds.STANDARD AIRPLANE WEIGHTSStandard Empty Weight . . . . . . . . . 1924 POUNDSMaximum Useful Load , Normal Category . . . . . . 1186 POUNDSCABIN AND ENTRY DIMENSIONSDetailed dimensions of the cabin interior and entry door openings areillustrated in Section 6.BAGGAGE SPACE AND ENTRY DIMENSIONSDimensions of the baggage area and baggage door opening areillustrated in detail in Section 6.SPECIFIC LOADINGSW ing Loading . . . . . . . . . . . . . . . 17.8 Ibs/sq. ft.Power Loading . . . . . . . . . . . . . . . . 13.5 Ibs/hp1-8U.S.182TPHBUS-00
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALSYMBOLS, ABBREVIATIONS AND TERMINOLOGYGENERAL AIRSPEED TERMINOLOGY AND SYMBOLSKCASKnots Calibrated Airspeed is indicated airspeed correctedfor position and instrument error and expressed in knots.Knots calibrated airspeed is equal to KTAS in standardatmosphere at sea level.KIASKnots Indicated Airspeed is the speed shown on theairspeed indicator and expressed in knots.KTASKnots True Airspeed is the airspeed expressed in knotsrelative to undisturbed air which is KCAS corrected foraltitude and temperature.Maneuvering Speed is the maximum speed at which full orabrupt control movements may be used withoutoverstressing the airframe.Maximum Flap Extended Speed is the highest speedpermissible with wing flaps in a prescribed extendedposition.Maximum Structural Cruising Speed is the speed thatshould not be exceeded except in smooth air, then only withcaution .Never Exceed Speed is the speed limit that may not beexceeded at any time.Stalling Speed or the minimum steady flight speed is theminimum speed at which the airplane is controllable.VsoStalling Speed or the minimum steady flight speed is theminimum speed at which the airplane is controllable in thelanding configuration at the most forward center of gravity.Best Angle of Climb Speed is the speed which results in thegreatest gain of altitude in a given horizontal distance .VyBest Rate of Climb Speed is the speed which results in thegreatest gain in altitude in a given time.(Continued Next Page)182TPHBUS-01U.S.1-9
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALSYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)METEOROLOGICAL utside Air Temperature is the free air statictemperature. It may be expressed in either degreesCelsius or degrees Fahrenheit.Standard Temperature is 15 C at sea level pressurealtitude and decreases by 2 C for each 1000 feet ofaltitude.Pressure Altitude is the altitude read from analtimeter when the altimeter's barometric scale hasbeen set to 29.92 inches of mercury (1013 mb).ENGINE POWER TERMINOLOGYBHPBrake Horsepower is the power developed by theengine.RPMRevolutions Per Minute is engine speed.StaticRPMStatic RPM is engine speed attained during a fullthrottle engine runup when the airplane is on theground and stationary.MPManifold Pressure is a pressure measured in theengine's induction system and is expressed in inchesof mercury (in .hg .).MCPMaximum Continuous Power(Continued Next Page)1-10U.S.182TPHBUS-00
CESSNAMODEL 182T NAV IIIGFC 700 AFCSSECTION 1GENERALSYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)ENGINE POWER TERMINOLOGY fFullThrottleClosedThrottleDecreased proportion of fuel in the fuel-air mixturesupplied to the engine. As air density decreases, theamount of fuel required by the engine decreases for agiven throttle setting. Adjusting the fuel-air mixture toprovide a smaller portion of fuel is known as "leaning"the mixture.Increased proportion of fuel in the fuel-air mixturesupplied to the engine. As air density increases, theamount of fuel required by the engine increases for agiven throttle setting. Adjusting the fuel-air mixture toprovide a greater portion of fuel is known as"richening" the mixture.Mixture control full forward (pushed in, full controltravel, toward the panel).Mixture control full aft (pulled out, full control travel,away from the panel).Throttle full forward (pushed in , full control travel ,toward the panel) . Also known as "full open" throttle.Throttle full aft (pulled out, full control travel, awayfrom the panel). Also known as the throttle "idle"position .(Continued Next Page)I 182TPHBUS-01U.S.1-11
CESSNAMODEL 182T NAV II IGFC 700AFCSSECTION 1GENERALSYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)AIRPLANE PERFORMANCE ANDTERMINOLOGYDemonstratedCrosswindVelocityUsable FuelFLIGHT PLANNINGDemonstrated Crosswind Velocity is the velocity ofthe crosswind component for which adequate controlof the airplane during takeoff and landing was actuallydemonstrated during certification tests. The valueshown is not considered to be limiting.Usable Fuel is the fuel available for flight planning.Unusable Fuel Unusable Fuel is the quantity of fuel that can not besafely used in flight.GPHGallons Per Hour is the amount of fuel consumed perhour.NMPGNautical Miles Per Gallon is the distance which canbe expected per gallon of fuel consumed at a specificengine power setting and/or flight configuration .g9 is acceleration due to gravity.Course Datum Course Datum is the compass reference used by theautopilot, along with course deviation, to provide lateralcontrol when tracking a navigation signal.(Continued Next Page)11-12U.S.182TPHBUS-01
SECTION 1GENERALCESSNAMODEL 182T NAV IIIGFC 700 AFCSSYMBOLS, ABBREVIATIONS AND TERMINOLOGY(Continued)WEIGHT AND BALANCE TERMINOLOGYReferenceDatumReference Datum is an imaginary vertical plane fromwh ich all horizontal distances are measured forbalance purposes.StationStation is a location along the airplane fuselage givenin terms of the distance from the reference datum.ArmArm is the horizontal distance from the referencedatum to the center of gravity (C.G.) of an item .MomentMoment is the product of the weight of an itemmultiplied by its arm . (Moment divided by the constant1000 is used in this POH to simplify
PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL CESSNA MODEL 182T NAV III AVIONICS OPTION -GFC 700 AFCS SERIALS 18281869 AND 18281876 AND ON ORIGINAL ISSUE -27 OCTOBER 2006 REVISION 3 -22 NOVEMBER 2010 PART NUMBER: 182TPHBUS-03 182TPHBUS-03 U.S. ilii . CESSNA INTRODUCTION MODEL 182T NAV III GFC 700 AFCS CONGRATULATIONS Congratulations on your purchase and welcome to Cessna .
